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- #~~~~~~~~~~~~~~~~~~~~~OUTPUT OF SUPER-CALCULATE (starts from your inputs) OPERATION (for further iteration use SUPER-ITERATE)~~~~~~~~~~~~~~~~~~~~~~~~
- #
- #
- #*******ANALYST: Prof. ULBaUser; TEST License: Professional*******
- #
- # Solution logged at: Aug 20, 2013 10:32:00 PM
- #
- #*******TEST-code: To save the solution, copy the codes generated below into a text file. To reproduce the solution at a later time, launch
- # the daemon (see path name below), paste the saved TEST-code at the bottom of this I/O panel, and click the Load button.
- #
- # Daemon Path: Systems>Open>SteadyState>Generic>SingleFlow>PG-Model; v-10.ae01
- #
- #--------------------Start of TEST-code-----------------------------------------------------------------------------
- States {
- State-1: Air;
- Given: { p1= 100.0 kPa; T1= 0.0 deg-C; Vel1= 0.0 m/s; z1= 0.0 m; mdot1= 0.4 kg/s; }
- State-2: Air;
- Given: { p2= "5*p1" kPa; h2= 175.18425 kJ/kg; Vel2= 0.0 m/s; z2= 0.0 m; mdot2= 0.4 kg/s; }
- State-3: Air;
- Given: { p3= "p2" kPa; T3= 35.0 deg-C; Vel3= 0.0 m/s; z3= 0.0 m; mdot3= 0.4 kg/s; }
- State-4: Air;
- Given: { p4= "p2" kPa; T4= 8.126 deg-C; Vel4= 0.0 m/s; z4= 0.0 m; mdot4= 0.4 kg/s; }
- State-5: Air;
- Given: { p5= "p1" kPa; T5= -80.0 deg-C; Vel5= 0.0 m/s; z5= 0.0 m; mdot5= 0.4 kg/s; }
- State-6: Air;
- Given: { p6= "p5" kPa; h6= -52.04 kJ/kg; Vel6= 0.0 m/s; z6= 0.0 m; mdot6= 0.4 kg/s; }
- State-7: Air;
- Given: { p7= "p2" kPa; s7= "s1" kJ/kg.K; Vel7= 0.0 m/s; z7= 0.0 m; mdot7= "0.4" kg/s; }
- State-8: Air;
- Given: { p8= "p1" kPa; T8= "T4" deg-C; Vel8= 0.0 m/s; z8= 0.0 m; mdot8= "0.4" kg/s; }
- State-9: Air;
- Given: { p9= "p4" kPa; T9= "T6" deg-C; Vel9= 0.0 m/s; z9= 0.0 m; mdot9= 0.4 kg/s; }
- }
- #----------------------End of TEST-code---------------------------------------------------------------------------------
- #
- #******DETAILED OUTPUT: All the computed properties and variables are displayed on this block.*************
- #
- # Evaluated States:
- #
- # State-1: Air > PG-Model;
- # Given: p1= 100.0 kPa; T1= 0.0 deg-C; Vel1= 0.0 m/s;
- # z1= 0.0 m; mdot1= 0.4 kg/s;
- # Calculated: v1= 0.7839 m^3/kg; u1= -103.4777 kJ/kg; h1= -25.0874 kJ/kg;
- # s1= 6.7988 kJ/kg.K; e1= -103.4777 kJ/kg; j1= -25.0874 kJ/kg;
- # Voldot1= 0.3136 m^3/s; A1= 31356.148 m^2; MM1= 28.97 kg/kmol;
- # R1= 0.287 kJ/kg.K; c_p1= 1.0035 kJ/kg.K; c_v1= 0.7165 kJ/kg.K;
- # k1= 1.4005 UnitLess;
- #
- # State-2: Air > PG-Model;
- # Given: p2= "5*p1" kPa; h2= 175.18425 kJ/kg; Vel2= 0.0 m/s;
- # z2= 0.0 m; mdot2= 0.4 kg/s;
- # Calculated: T2= 199.5743 deg-C; v2= 0.2713 m^3/kg; u2= 39.5187 kJ/kg;
- # s2= 6.8873 kJ/kg.K; e2= 39.5187 kJ/kg; j2= 175.1842 kJ/kg;
- # Voldot2= 0.1085 m^3/s; A2= 10853.24 m^2; MM2= 28.97 kg/kmol;
- # R2= 0.287 kJ/kg.K; c_p2= 1.0035 kJ/kg.K; c_v2= 0.7165 kJ/kg.K;
- # k2= 1.4005 UnitLess;
- #
- # State-3: Air > PG-Model;
- # Given: p3= "p2" kPa; T3= 35.0 deg-C; Vel3= 0.0 m/s;
- # z3= 0.0 m; mdot3= 0.4 kg/s;
- # Calculated: v3= 0.1769 m^3/kg; u3= -78.4 kJ/kg; h3= 10.0349 kJ/kg;
- # s3= 6.4579 kJ/kg.K; e3= -78.4 kJ/kg; j3= 10.0349 kJ/kg;
- # Voldot3= 0.0707 m^3/s; A3= 7074.792 m^2; MM3= 28.97 kg/kmol;
- # R3= 0.287 kJ/kg.K; c_p3= 1.0035 kJ/kg.K; c_v3= 0.7165 kJ/kg.K;
- # k3= 1.4005 UnitLess;
- #
- # State-4: Air > PG-Model;
- # Given: p4= "p2" kPa; T4= 8.126 deg-C; Vel4= 0.0 m/s;
- # z4= 0.0 m; mdot4= 0.4 kg/s;
- # Calculated: v4= 0.1614 m^3/kg; u4= -97.6554 kJ/kg; h4= -16.933 kJ/kg;
- # s4= 6.3663 kJ/kg.K; e4= -97.6554 kJ/kg; j4= -16.933 kJ/kg;
- # Voldot4= 0.0646 m^3/s; A4= 6457.794 m^2; MM4= 28.97 kg/kmol;
- # R4= 0.287 kJ/kg.K; c_p4= 1.0035 kJ/kg.K; c_v4= 0.7165 kJ/kg.K;
- # k4= 1.4005 UnitLess;
- #
- # State-5: Air > PG-Model;
- # Given: p5= "p1" kPa; T5= -80.0 deg-C; Vel5= 0.0 m/s;
- # z5= 0.0 m; mdot5= 0.4 kg/s;
- # Calculated: v5= 0.5543 m^3/kg; u5= -160.7983 kJ/kg; h5= -105.3669 kJ/kg;
- # s5= 6.451 kJ/kg.K; e5= -160.7983 kJ/kg; j5= -105.3669 kJ/kg;
- # Voldot5= 0.2217 m^3/s; A5= 22172.58 m^2; MM5= 28.97 kg/kmol;
- # R5= 0.287 kJ/kg.K; c_p5= 1.0035 kJ/kg.K; c_v5= 0.7165 kJ/kg.K;
- # k5= 1.4005 UnitLess;
- #
- # State-6: Air > PG-Model;
- # Given: p6= "p5" kPa; h6= -52.04 kJ/kg; Vel6= 0.0 m/s;
- # z6= 0.0 m; mdot6= 0.4 kg/s;
- # Calculated: T6= -26.8588 deg-C; v6= 0.7068 m^3/kg; u6= -122.7223 kJ/kg;
- # s6= 6.6949 kJ/kg.K; e6= -122.7223 kJ/kg; j6= -52.04 kJ/kg;
- # Voldot6= 0.2827 m^3/s; A6= 28272.902 m^2; MM6= 28.97 kg/kmol;
- # R6= 0.287 kJ/kg.K; c_p6= 1.0035 kJ/kg.K; c_v6= 0.7165 kJ/kg.K;
- # k6= 1.4005 UnitLess;
- #
- # State-7: Air > PG-Model;
- # Given: p7= "p2" kPa; s7= "s1" kJ/kg.K; Vel7= 0.0 m/s;
- # z7= 0.0 m; mdot7= "0.4" kg/s;
- # Calculated: T7= 159.6605 deg-C; v7= 0.2484 m^3/kg; u7= 10.9202 kJ/kg;
- # h7= 135.131 kJ/kg; e7= 10.9202 kJ/kg; j7= 135.131 kJ/kg;
- # Voldot7= 0.0994 m^3/s; A7= 9936.862 m^2; MM7= 28.97 kg/kmol;
- # R7= 0.287 kJ/kg.K; c_p7= 1.0035 kJ/kg.K; c_v7= 0.7165 kJ/kg.K;
- # k7= 1.4005 UnitLess;
- #
- # State-8: Air > PG-Model;
- # Given: p8= "p1" kPa; T8= "T4" deg-C; Vel8= 0.0 m/s;
- # z8= 0.0 m; mdot8= "0.4" kg/s;
- # Calculated: v8= 0.8072 m^3/kg; u8= -97.6554 kJ/kg; h8= -16.933 kJ/kg;
- # s8= 6.8282 kJ/kg.K; e8= -97.6554 kJ/kg; j8= -16.933 kJ/kg;
- # Voldot8= 0.3229 m^3/s; A8= 32288.97 m^2; MM8= 28.97 kg/kmol;
- # R8= 0.287 kJ/kg.K; c_p8= 1.0035 kJ/kg.K; c_v8= 0.7165 kJ/kg.K;
- # k8= 1.4005 UnitLess;
- #
- # State-9: Air > PG-Model;
- # Given: p9= "p4" kPa; T9= "T6" deg-C; Vel9= 0.0 m/s;
- # z9= 0.0 m; mdot9= 0.4 kg/s;
- # Calculated: v9= 0.1414 m^3/kg; u9= -122.7223 kJ/kg; h9= -52.04 kJ/kg;
- # s9= 6.2331 kJ/kg.K; e9= -122.7223 kJ/kg; j9= -52.04 kJ/kg;
- # Voldot9= 0.0566 m^3/s; A9= 5654.5806 m^2; MM9= 28.97 kg/kmol;
- # R9= 0.287 kJ/kg.K; c_p9= 1.0035 kJ/kg.K; c_v9= 0.7165 kJ/kg.K;
- # k9= 1.4005 UnitLess;
- #
- #--------Property spreadsheet starts: The following property table can be copied onto a spreadsheet (such as Excel) for further analysis or plots. ---------------
- #
- # State p(kPa) T(K) v(m^3/kg) u(kJ/kg) h(kJ/kg) s(kJ/kg)
- # 1 100.0 273.2 0.7839 -103.48 -25.09 6.799
- # 2 500.0 472.7 0.2713 39.52 175.18 6.887
- # 3 500.0 308.2 0.1769 -78.4 10.03 6.458
- # 4 500.0 281.3 0.1614 -97.66 -16.93 6.366
- # 5 100.0 193.1 0.5543 -160.8 -105.37 6.451
- # 6 100.0 246.3 0.7068 -122.72 -52.04 6.695
- # 7 500.0 432.8 0.2484 10.92 135.13 6.799
- # 8 100.0 281.3 0.8072 -97.66 -16.93 6.828
- # 9 500.0 246.3 0.1414 -122.72 -52.04 6.233
- #
- #--------Property spreadsheet ends--------------------------------------------------------------------
- #
- #******CALCULATE VARIABLES: Type in an expression starting with an '=' sign ('= mdot1*(h2-h1)', '= sqrt(4*A1/PI)', etc.) and press the Enter key)*********
- #
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